# STC SA4388SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC pitch stabilization system Model ST-052 with Optional autotrim system
- Status date: April 6, 1982
- Data sheets: 3A15, 3A15, 3A15
- Certificate PDF: https://openairdocs.org/files/sha256/ef/31/ef319ce9b93825ce5752a904c23518ac3815ce6294c0e9b49badd30f38fe753d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/614434F18538D73986257E030053405C.0001
- Page: https://openairdocs.org/stc/SA4388SW

## ADs that name it

None.

## Approved models (3)

- Beechcraft Corporation 36 (TCDS 3A15)
- Beechcraft Corporation A36 (TCDS 3A15)
- Beechcraft Corporation F33A (TCDS 3A15)

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

£t«ts of amtrica tst&OMta& Bepartment ontransportation— Jfederal atriation administration Supplemental 'Cgpe Certificate AS / iSKwmvev SA4388SW Project A5729SW-DS FKP-190 S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067-9990 ^^^&^e>6tc>tv^^ JfoM/r<v(^ 3 ^J&v Civil Air 3A15 Beech 36, A36, F33A, S/N CE-316 and UP Installation of S-TEC Pitch Stabilization System, Model ST-052 with Optional Autotrim System according to Bulletin No. 155, Revision 2, dated 3-01-82 and Master Drawing list No. 9250, dated 3-01-82, or later FAA approved revision.

(14 volt system) : See Continuation Sheet, page 2 of this STC.

<w SXcfm^fnji^fa^f-^^A« May 15, 1981 June 19, 1981 : 9/22/81; 4/6/82 Revision 2 Don P. Watson^Manager, Aircraft Certification Division Southwest Region (Title)

This certificate may be transferred in accordance with FAR 21.17.

ttnittd Starts of America Btpartmcnt of Transportation— federal atoiation administration ^uppltmtntal 7Cgpe Certificate(Continuation £hett) SA4388SW Revision 2 Limitations and Conditions:

1. Pilotis Operating Handbook and FAA Approved Airplane Flight Manual Supplement, P/N 8953 dated June 19, 1981, is required for Beech Models 36, A36, F33A, S/N CE-511 and UP with S-TEC System 60 Pitch Stabilization System, Model ST-052 without optional autotrim system; OR Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement, P/N 8953-1 dated September 22, 1981, is required for Beech Models 36, A36, F33A, S/N CE-511 and UP with S-TEC System 60 Pitch Stabilization System, Model ST-052 with or without optional autotrim system; OR FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8953-2 dated April 6, 1982, is required for Beech Models 36, A36, F33A, S/N CE-316 and UP.

2. Compatibility of this modification with other previously approved modifications must be determined by the installer.

Anr alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding .3 years, or hulk.

KAA FORM 8110-2-1 (1O-69) This certificate may be trarx/errtd in accordance with FAR J.V.-/.7.

PAGE 2°F2 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) Number and street) (City, State, and £IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ^IP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- April 6, 1982: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ef/31/ef319ce9b93825ce5752a904c23518ac3815ce6294c0e9b49badd30f38fe753d)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.